推进技术 ›› 1989, Vol. 10 ›› Issue (1): 14-18.
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张铭玉
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摘要： 根据火箭发动机的推力公式及空气动力学有关理论,导出在小斜切角喷管内气体流动的特性、推力的变化规律,并给出喷管的设计方法.
关键词: 斜置喷管;推力;近似计算;火箭发动机喷管
Abstract: In this paper, the aerodynamic performance and the thrust performance of the small bevel nozzle of rocket engines are developed based on thrust equation of rocket engines and theories in aerodynamics. A design method of this kind of nozzles is also presented.
Key words: Canted nozzle;Thrust;Approximate;calculation;Roeket enginenozzle
张铭玉. 火箭发动机小斜切角喷管的设计方法[J]. 推进技术, 1989, 10(1): 14-18.
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